U.S. patent number 3,772,566 [Application Number 05/141,134] was granted by the patent office on 1973-11-13 for linearization of magnetically deflected cathode ray tube with non-axial guns.
This patent grant is currently assigned to Loral Corporation. Invention is credited to Jacob H. Schwartz.
United States Patent |
3,772,566 |
Schwartz |
November 13, 1973 |
LINEARIZATION OF MAGNETICALLY DEFLECTED CATHODE RAY TUBE WITH
NON-AXIAL GUNS
Abstract
Linearization means permitting the use of a plurality of
magnetically deflected electron guns within a single Cathode-Ray
Tube in which at least one of the guns is displaced from the
longitudinal tube or screen axis, and in which the yoke deflection
currents are compensated to allow proper registration between
images formed by separate guns. The corrective function, for a
laterally displaced gun, which is mathematically complex is
simplified to a form more readily produced by a function generator,
and is used to modify the uncorrected deflection voltages which
control the beam deflection currents. A means for extending this
technique to electron guns which are not parallel to the
longitudinal or screen axis is also provided.
Inventors: |
Schwartz; Jacob H. (Bronx,
NY) |
Assignee: |
Loral Corporation (Scarsdale,
NY)
|
Family
ID: |
22494304 |
Appl.
No.: |
05/141,134 |
Filed: |
May 7, 1971 |
Current U.S.
Class: |
315/370;
348/E3.048; 348/E3.045; 315/382; 315/393 |
Current CPC
Class: |
G06G
7/22 (20130101); H04N 3/2335 (20130101); H04N
3/26 (20130101) |
Current International
Class: |
G06G
7/22 (20060101); G06G 7/00 (20060101); H04N
3/233 (20060101); H04N 3/26 (20060101); H04N
3/22 (20060101); H01j 029/70 () |
Field of
Search: |
;315/27GD,27TD,31R,24 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Padgett; Benjamin R.
Assistant Examiner: Potenza; J. M.
Claims
I claim:
1. A circuit for providing correctional voltages whereby in a
magnetically deflected multi-gun cathode-ray tube, an electron gun
having a principal axis laterally displaced with respect to a
principal screen axis may be linearized with respect to said
principal axis, said circuit comprising: X and Y signal position
inputs, first and second squaring circuits connected respectively
to said X and Y signal position inputs, a summing amplifier summing
the outputs of said squaring circuits and a position input
coordinate Y.sub.1 corresponding to the direction of gun
displacement, to produce the synthetic variable:
R = X.sup.2 + PY.sup.2 + QY
where X and Y are input coordinates system variables, P is a
constant approximated by the relation
P .apprxeq. 1 - [ n sin .mu./n cos .mu. - 1].sup.2
Qis a constant approximated by the relation
Q .apprxeq. 2R.sub.1 (n sin .mu./n cos .mu. - 1)
and optimized to produce best linearity
R.sub.1 = the distance along the undeflected electron beam between
the center of deflection and the screen,
.mu. = arc sin Y/R.sub.2,
R.sub.2 = the radius of screen curvature,
Y = the distance through which the gun is displaced from the screen
axis
n = R.sub.2 /R.sub. 1,
a function generator connected to the output R of said summing
amplifier, and generating an optimized but simplified corrective
function G-1, where G approximates the true but complex function:
##SPC3##
multiplier means connected to the output of said function generator
and said signal position inputs producing a product proportional to
the correction voltage required, and means summing the corrective
voltage and the deflection voltage.
2. Structure in accordance with claim 1, including scaling means
connected to said function generator to provide a dynamic focus
correction signal.
3. Structure in accordance with claim 1, including rotational
coordinate conversion means comprising a pair of summing amplifiers
and an inverter interconnecting the said position inputs and said
squaring circuits.
4. A circuit for providing correctional voltages whereby an
electron gun having a principal axis which is not parallel to the
principal screen axis may be linearized with respect to said
principal axis, by simulating a laterally displaced gun with the
same center of deflection as the actual tilted gun, said circuit
comprising: X.sub.t and Y.sub.t signal position inputs with respect
to the tilted gun, X.sub.o and Y.sub.o constant incremental
coordinate inputs corresponding to the coordinates of the actual
undeflected spot with respect to the simulated gun coordinates,
summing means to add the incremental coordinates to the inputs
producing the simulated coordinates X.sub.t + X.sub.o and Y.sub.t +
Y.sub.o, a linearization circuit designed for the simulated
laterally displaced gun according to claim 1, accepting said
simulated coordinates as inputs and providing the corrected
deflection outputs G(X.sub.t + X.sub.o) and G(Y.sub.t + Y.sub.o)
for the simulated electron gun and the dynamic focus correction,
first and second squaring circuits connected to said corrected
deflection outputs, a summing amplifier to subtract the outputs of
said squaring circuits from the constant R.sub.1.sup.2, a square
root circuit connected to the output of said summing amplifier to
develop the term .sqroot.R.sub.1.sup.2 - G.sup.2 [(X.sub.t +
X.sub.o).sup.2 + (Y.sub.t + Y.sub.o).sup.2 ] and summing means with
appropriate scaling connected to the output of said square root
circuit and the deflection outputs G(X.sub.t + X.sub.o) and
G(Y.sub.t + Y.sub.o) of the linearization circuit to produce the
corrected deflection outputs for the actual tilted gun such
that
X output = G(X.sub.t + X.sub.o) - U sin .phi.
Y output = G(Y.sub.t + Y.sub.o) - U cos .phi.
where U = (1 - cos .delta.)(G(X.sub.t + X.sub.o) sin .phi. +
G(Y.sub.t + Y.sub.o) cos .phi.) .sup.+ .sqroot.R.sub.1.sup.2 -
G.sup.2 [(X.sub.t + X.sub.o).sup.2 + (Y.sub.t + Y.sub.o).sup.2 ]
sin .delta.
.phi. = angle with repsect to vertical of plane in which gun is
tilted
and .delta. = angle of tilt of actual electron gun.
5. Structure in accordance with claim 4, in which linearization
correction for any non-axial electron gun is developed in terms of
a simulated electron gun with the same center of deflection as the
tilted gun but with principal axis parallel to the screen principal
axis, the resulting correction signals subsequently being converted
to the form required for the actual tilted gun in terms of the
angles .phi. and .delta., defining the orientation of the tilted
gun with respect to the simulated gun.
Description
This invention relates to magnetically deflected cathode-ray tube
(CRT) displays which are required to present a great variety of
information (from many diverse sources) simultaneously on a single
cathode-ray tube, at normal refresh rates, and more particularly to
an improved linearization circuit for use in correcting the
deflection of the electron beam from any of a plurality of guns
which is mounted in offset relation with respect to the principal
tube or screen axis.
As the amount of information to be displayed on a single gun
cathode-ray tube increases, a point is soon reached where
considerations of writing speed, brightness and flicker bring about
a condition of saturation of the data processing capability of the
tube. Clearly, this information display capability can be extended
(at a rate of 100 percent per electron gun) if additional guns are
added within the cathode-ray tube envelope. However, since physical
constraints limit the minimum separation between electron guns to
about 3 inches (to allow adequate space for separate deflection
coils) and only one electron gun can be mounted axially with the
cathode ray tube screen, a severe linearity problem is created for
the off-axis electron guns. Moreover, without good linearity,
registration between images produced by the separate guns is poor,
and the advantage of any additional electron guns within the
cathode-ray tube envelope is lost.
It is therefore among the principal objects of the present
invention to provide an improved electronic circuit for providing a
corrective signal to modify the normal deflection voltage for a
given gun, whereby proper linearity is obtained.
Another object of the invention lies in the provision of circuitry
as above described, in which the corrective function produced by
circuit is relatively simple to generate, as contrasted with an
exact function of greater complexity.
These objects, as well as other incidental ends and advantages,
will more fully appear in the progress of the following disclosure,
and be pointed out in the appended claims.
In the drawing, to which reference will be made in the
specifications:
FIG. 1 is a graph comparing the characteristics of the exact
parallel offset gun deflection signal correction factor G in terms
of spot deflection distance R, and a close, readily generated
approximation of this function in terms of a systhetic variable R
for a typical rectangular CRT screen size.
FIG. 2 is a schematic block diagram of a circuit embodying the
invention as applied to a parallel offset gun.
FIG. 3 is a vector diagram, showing the position of an alternate
system of coordinates for use where a given additional gun is
laterally displaced to a position other than along either the X or
the Y coordinate axis of the screen.
FIG. 4 is a perspective drawing, illustrating the deflection
geometry for a non-axial gun CRT.
FIG. 5 is a schematic block diagram of a circuit embodying the
invention as applied to a tilted electron gun.
Briefly stated, the invention comtemplates the provision of a
circuit which will supply small corrective voltages added to the
uncorrected deflection voltages for any gun of a multi-gun
cathode-ray tube, whereby linearity with respect to a plane
perpendicular to the screen axis is obtained. As a true corrective
function is difficult to generate, a simplification, more readily
producable is substituted therefore, this function being multiplied
by the uncorrected deflection voltages, and added to the same to
provide corrected deflection voltages.
Before entering into a detailed consideration of the structural
aspects of the invention, a review of the theory of operation is
considered apposite.
With magnetic beam deflection, the relation between deflection
current I (in the deflection yoke) and electron beam deflection
angle .gamma. is given by I = K sin .gamma., where K is a constant
of proportionality. If the cathode-ray tube screen radius of
curvature is R.sub.2, and the electron gun is displaced parallel to
the screen axis (defined as a line perpendicular to the cathode-ray
tube screen at its center) a distance y along the negative Y
display axis, then the angle at which the undeflected electron beam
impinges upon the screen is 90.degree.-.mu., where .mu. = arc sin
Y/R.sub.2. If the distance along the undeflected electron beam
between the center of deflection and the screen is R.sub.1, and the
uncorrected horizontal and vertical deflection currents (I.sub.x
and I.sub.y, respectively) are modified by the correction function
G where ##SPC1##
and n= R.sub.2 /R.sub.1, the deflection sensitivity for this offset
gun (with respect to a plane perpendicular to the undeflected
electron beam) will remain constant over the entire cathode ray
tube screen area.
The function G above is exact, but since it is dependent upon both
the horizontal and vertical deflection inputs, it is very difficult
to generate. A great simplification occurs if it were possible to
redefine the function in terms of a single, easily obtainable,
variable. Such a transformation, in accordance with the invention,
has been obtained. A new variable R is synthesized, where
R = [(Ix).sup.2 /K + P(Iy).sup.2 /K + Q/R.sub.1 . Iy/k ]
R.sub.1.sup.2
and P and Q are constants which may be approximated by the
relations
P .apprxeq. 1 - [(n sin .mu.)/(n cos .mu. -1)].sup.2
Q .apprxeq. 2R.sub.1 (n sin .mu.)/(n cos .mu.- 1)
The value of P is almost unity. The value of Q must be optimized
for best overall display accuracy, using the relation given above
as a starting point. In a more sophisticated design, the value of Q
may be permitted to vary slightly as a function of R (using
feedback or stepped levels.). Making the substitutions I.sub.x /K =
X/R.sub.1, and I.sub.y /K=Y/R.sub.1 (where X and Y are the
instantaneous spot deflection coordinates) we may rewrite R as
R = X.sup.2 + P Y.sup.2 + Q Y
and G as ##SPC2##
The design method consists of selecting a test value for Q and, for
a number of equally spaced values of R over the range of interest,
determining the boundary values for both x and Y at each R. The
values of G at these boundary points are then computed giving the
maximum spread in G value at each R. The value of Q is readjusted
until a minimum spread in the G function over the entire range of R
is achieved. The G function generator is designed to reproduce the
mean values of the optimized band function obtained above as a
function of R.
A plot of the function G versus R is illustrated in FIG. 1. Also
plotted is the function G versus R where
R = .sqroot.X.sup.2 + Y.sup.2
It is clear from this figure that the use of the synthetic variable
R makes possible the collapse of the area function G into an easily
generated, almost linear, line function. The variable R is derived
from the X and Y position input signals by means of a pair of
squaring circuits and a summing amplifier.
For simplicity, the discussion above is limited to the case of an
electron gun offset along the Y coordinate axis. This may now be
generalized to apply to a gun offset at any point on the
cathode-ray tube screen, but with the electron gun axis maintained
parallel to the screen axis. Assume that the gun is offset a
distance y' from the screen axis (center) in a direction making an
angle .theta. with respect to the deflection vertical (Y) axis. If
the electron beam is deflected through a deflection angle .gamma.
in a given plane of deflection, it can be demonstrated that the
applicable value of the correction function G is fixed and is
independent of the coordinate system which was used to cause the
beam deflection. Hence, any coordinate system may be used to derive
the value of G.
If the position deflection input coordinate system is X,Y, a
rotation of coordinates through the angle is performed to obtain
the new coordinate system X', Y', where the Y' axis intersects the
screen axis. (See FIG. 3.) The equations for the correction
function G and the synthetic variable R given above, may be used
directly for the coordinate system X', Y', after the substitution
of X' for X and Y' for Y. The values of the position coordinates X'
and Y' are obtained from the input position coordinates X and Y by
use of the coordinate rotation equations
X '= X cos .theta. - Y sin .theta.
Y '= X sin .theta. + Y cos .theta.
The values of sin .theta. and cos .theta. are constant for a
specified gun position and .mu. = arc sin y'/R.sub.2 for this case.
Therefore, the circuit design for this generalized gun position
case is identical to that for the simplified case with the addition
of a standard coordinate rotation section.
Alternatively, if a slight reduction in accuracy is acceptable, the
value of P may be set to unity making R=X.sup.2 + Y.sup.2 + QY cos
.theta. + QX sin .theta. and eliminating the need for coordinate
conversion.
With the foregoing discussion in mind, reference may now be made to
a block diagram of an offset gun cathode-ray tube deflection
linearization circuit embodying the invention for the generalized
case shown in FIG. 2. Coordinate conversion is accomplished using a
pair of summing amplifiers and an inverter. If the coordinate
rotation angle .theta. is zero, or some multiple of 90.degree.,
this structure may be liminated. The value of R is synthesized from
the X' and Y' coordinates using a pair of squaring circuits and a
summing amplifier. The remainder of the circuit operates with the
original position coordinates X and Y. Since the correction
function G varies over a small range, the linearity correction
function generator is designed to generate the magnitude G- 1
corresponding to the input value of R. The quantity G - 1 is then
multiplied by each of the two position inputs, producing the
correction terms GX -X and GY Y, which, when added to the
corresponding uncorrected inputs produces the corrected position
signals GX and GY, respectively. Since the corrected position
signals are obtained by the summation of small correction terms to
the actual position inputs, any errors in the linearity circuit are
reduced by almost an order of magnitude in terms of full scale
deflection output. The almost linear relationship between G and R
assures minimum distortion of displayed conic figures and vectors,
since the function generator breakpoint slope transitions can be
kept shallow. The disclosed deflection linearization circuit also
generates the cathode-ray tube dynamic focus correction signal
which is extracted by simply rescaling the G - 1 signal.
Thus, the circuit, generally indicated by reference character 10,
includes X and Y position inputs 11 and 12, as well as inverter 13
and summing amplifiers 14 and 15, the last three elements being
optionally deletable. The summing amplifiers feed squaring circuits
16 and 17, the outputs of which in combination with the unsquared
input to 17 are fed to a summing amplifier 18 to generate the
synthetic variable R. This in turn is connected to the function
generator 19 which generates the above described function G - 1.
The output of the function generator 19 is fed to multipliers 20
and 21 where the function is multiplied by the deflection voltages
from the inputs 11 and 12, and the products are summed with these
same inputs in amplifiers 22 and 23 producing the required
corrected position signals GX and GY. A scaling device 24 is also
driven by the function generator 19 to provide a dynamic focus
correction signal in a manner more fully described and claimed in
my copending application Ser. No. 103,374, filed Jan. 4, 1971.
A computer analysis of the disclosed linearization technique shows
that the maximum theoretical spot position error can be suppressed
to within 3 mils for a 15 inch diagonal cathode-ray tube with gun
position offset by 1.5 inches from the screen center.
The technique disclosed above may be extended to the still more
general case of an electron gun which is not parallel to the screen
axis, by simulating an imaginary electron gun which is parallel to
the screen axis and which operates through the same center of
deflection as the actual non-paralled electron gun. If the distance
R.sub.B (along the actual undeflected beam) between the center of
deflection and the point where the beam impinges on the CRT screen
is known, the value of R.sub.1 for the simulated parallel gun may
be computed for use in the expression for G. (see FIG. 4.) Since
the undeflected spot of the actual beam falls some distance away
from the zero position of the simulated electron gun, the
incremental deflection coordinates X.sub.o and Y.sub.o of the
actual undeflected spot with respect to the simulated gun
coordinate system must also be computed. The values of R.sub.1,
X.sub.o and Y.sub.o are constants for a given electron gun
configuration.
If the values of X.sub.o and Y.sub.o are added to the actual
X.sub.t and Y.sub.t position inputs, respectively, (where X.sub.t
and Y.sub.t are the instantaneous spot deflection coordinates for
the tilted gun) the required correction function G (or G - 1) may
be obtained directly using the circuit illustrated in FIG. 2, by
letting X= X.sub.t + X.sub.o and Y = Y.sub.t + Y.sub.o. The outputs
of this circuit would then be G (X.sub.t + X.sub.o) and G (Y.sub.t
+ Y.sub.o). These outputs, however, are not directly applicable to
the tilted gun deflection circuits without some additional
processing. If the position of the actual electron gun is tilted
upward through an angle .delta. with respect to the simulated
parallel gun in a plane which makes an angle .phi. counterclockwise
with respect to the vertical when viewed from the face of the CRT,
the required corrected X and Y deflection signals for the tilted
gun are:
X deflection = G(X.sub.t + X.sub.o)-[(1 - cos .delta.)(G(X.sub.t +
X.sub.o) sin .phi. + G (Y.sub.t + Y.sub.o) cos .phi.) .sup.+
.sqroot.R.sub.1.sup.2 - G.sup.2 [(X.sub.t + X.sub.o).sup.2+(Y.sub.t
+ Y.sub.o).sup.2 ]sin .delta.] sin .phi.
Y deflection = G(Y.sub.t + Y.sub.o) - [(1 - cos .delta.)(G(X.sub.t
+ X.sub.o) sin .phi. + G (Y.sub.t + Y.sub.o) cos .phi. .sup.+
.sqroot.R.sub.1.sup.2 - G.sup.2 [(X.sub.t + X.sub.o).sup.2 +
(Y.sub.t + Y.sub.o).sup.2 ] sin .delta.] cos .phi.
Since .delta. and .phi. are constants for a given electron gun, all
of the terms in these expressions are readily available except for
the term .sqroot.R.sub.1.sup.2 - G.sup.2 [(X.sub.t + X.sub.o).sup.2
+ (Y.sub.t + Y.sub.o).sup.2 ] which may be derived using standard
computing modules or, if accuracy limitations permit, by simpler
approximate means. For a flatfaced CRT screen this square root term
is simple R.sub.1 G. If the electron gun is tilted in one axis
only, e.g., .phi. = 0, X.sub.o = 0, the above expressions simplify
to:
X deflection = GX.sub.t
Y deflection = G(Y.sub.t + Y.sub.o) cos .delta. -
.sqroot.R.sub.1.sup.2 - G.sup.2 [X.sub.t.sup.2 + (Y.sub.t +
Y.sub.o).sup.2 ] sin .delta.
With the foregoing discussion in mind, reference may now be made to
a block diagram of a completely generalized non-axial and
non-parallel electron gun cathode-ray tube deflection linearization
circuit embodying the invention, shown in FIG. 5. Translation of
actual gun deflected spot coordinates X.sub.t, Y.sub.t to simulated
parallel gun coordinates X, Y is accomplished using a pair of
summing amplifiers which add the displacement coordinates of the
undeflected spot X.sub.o, Y.sub.o, with respect to the simulated
gun, to the input deflection signals. The summed signals are
applied as inputs to a linearization circuit designed for the
simulated parallel offset gun as described above and as illustrated
in FIG. 2. The dynamic focus correction output of this
linearization circuit may be used directly. The deflection outputs
G(X.sub.t + X.sub.o) and G(Y.sub.t + Y.sub.o) must be transposed
back to the coordinates of the actual gun. This is accomplished by
squaring the deflection signals and subtracting the results from
the constant R.sub.1.sup.2 using a pair of squaring circuits and a
summing amplifier. The square root of this signal is summed with
the deflection signals, using appropriate scaling, to develop the
correction term
-[(1 - cos .delta.)(G(X.sub.t + X.sub.o)sin .phi. + G(Y.sub.t +
Y.sub.o) cos .phi.)
.sup.+ .sqroot.R.sub.1.sup.2 - G.sup.2 [(X.sub.t + X.sub.o).sup.2 +
(Y.sub.t + Y.sub.o).sup.2 ] sin .delta.
where, as noted above, .delta. and .phi. are constants. This
correction term is added to the deflection signals G(X.sub.t +
X.sub.o) and G(Y.sub.t + Y.sub.o), with appropriate scaling, to
produce the required corrected X and Y deflection outputs for the
tilted gun.
Thus, the circuit, generally indicated by reference character 25,
includes X.sub.t and Y.sub.t position inputs 26 and 28,
displacement coordinate inputs X.sub.o, Y.sub.o of the undeflected
spot 27 and 29, and summing amplifiers 30 and 31 which feed a
linearization circuit 32, designed for a parallel offset gun (with
the same center of deflection as the actual tilted gun) according
to the method described earlier in this disclosure. The deflection
outputs of the linearization circuit G(X.sub.t + X.sub.o) and
G(Y.sub.t + Y.sub.o) are fed to squaring circuits 33 and 34, which
feed summing amplifier 35 where the squared deflection signals are
substracted from the constant R.sub.1.sup.2, followed by derivation
of the square root of this result in the square root circuit 36.
This square root signal is added to the deflection signals
G(X.sub.t + X.sub.o) and G(Y.sub.t + Y.sub.o), with appropriate
scaling, in summing amplifier 37 which feeds the final correction
signal to summing amplifiers 38 and 39 which also accept the
deflection signals G(X.sub.t + X.sub.o) and G(Y.sub.t + Y.sub.o),
respectively, to produce the required corrected X and Y deflection
outputs for the tilted gun. The linearization circuit 32 also
provides the dynamic focus correction signal which may be used
directly without further processing.
It may thus be seen that I have invented novel and highly useful
improvements in a cathode-ray tube deflection linearization circuit
for use with a laterally offset or tilted gun which provides a
simple, highly accurate, solution to a complex linearity problem.
The disclosed embodiment includes means for linearizing imagery
from independently deflected electron guns located anywhere within
the cathode-ray tube envelope, making possible the design of a
multi-gun cathode-ray tube display without serious registration
problems between separate superimposed images. Additionally, a
dynamic focus correction signal for each electron gun is provided
without additional computational hardware. Correction is
accomplished in a manner to incidently provide for minimum
distortion of displayed conics and vectors.
I wish it to be understood that I do not consider the invention
limited to the precise details of structure shown and set forth in
this specification, for obvious modifications will occur to those
skilled in the art to which the invention pertains.
* * * * *